We mainly research on fault detection of closed - loop control systems and adaptive reconfiguration control based on fault detection and its application on flight control systems 本文主要研究了闭环控制系统的故障检测和基于故障检测的自适应重构控制在飞行控制系统中的应用。
It can be seen that the structure and parameters of the flight control system are reasonable ; the performance can meet the need of the task 通过给出的部分仿真结果可以看出，本文得出的巡航式飞行器飞行控制系统结构合理，设计方法可靠，系统参数可以满足该飞行器控制的总体性能要求。
To shorten aircraft r & d time and reduce cost , simulation is necessary , aircraft is an airborne one and environmental actions on aircraft are simulated by the loading system 在仿真系统中，飞行控制系统采用实物，而飞行器在飞行过程中所受的外界作用力则由电液伺服加载系统来提供。
It is the important development to adopt the flight control system ( pcs ) to improve handling quality , and control law design plays an important role in helicopter handling quality design 采用飞行控制系统改善飞行品质是重要发展方向，控制律的设计是直升机飞行品质设计的重要内容。
Then a discussion is devoted to the design of a robust flight control system which is used to overcome the di sadvantage of the neural network based on disturbance observer 同时为了克服神经网络的硬件实现困难以及其自适应算法的复杂性，提出并设计了基于干扰观测器的鲁棒飞行控制系统。
At the end of the dissertation , the fuzzy pd track tail controller is designed . the pd controller and controller of attitude angle are made up of flight control system of helicopter 最后，本文设计了直升机模糊pd轨迹跟踪控制器，与姿态角控制器相结合，完成了对整个飞行控制系统的设计。
At last , the proposed methods are successfully applied to the simulation of fighter flight control system , results of simulation test show the effectiveness of the proposed methods 最后将文中所提出的方法成功地应用于歼击机飞行控制系统的数字仿真实验，仿真结果表明了本文方法的有效性。
The method of the non - fragile synthesis robust control was proposed for the design of common flight control system with the perturbations of the controlled members and the controllers 摘要为了解决在被控对象和控制器同时摄动时飞行控制系统的设计问题，提出了非脆弱综合鲁棒控制系统设计方法。
In the end of the paper , the lqt based on ga is applied to design the flight control system of rss uavs . the intensive simulation verified the validity of our research 最后，应用基于遗传算法的线性二次型跟踪器技术对放宽航向静稳定性无人机的飞行控制系统进行设计，试验结果验证了研究成果的有效性。
After that a control system of the unmanned helicopter in high stability was analyzed with the system principle and control law , with which the design task and its design rule was proposed 然后对高稳定性无人机飞行控制系统进行了系统原理分析和控制律原理分析,提出了设计任务以及应遵循的主要设计原则。
